CN105220308A - A kind of impact resistant composite material fabric - Google Patents

A kind of impact resistant composite material fabric Download PDF

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Publication number
CN105220308A
CN105220308A CN201510699630.7A CN201510699630A CN105220308A CN 105220308 A CN105220308 A CN 105220308A CN 201510699630 A CN201510699630 A CN 201510699630A CN 105220308 A CN105220308 A CN 105220308A
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China
Prior art keywords
composite material
impact resistant
resistant composite
material fabric
steel wire
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CN201510699630.7A
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CN105220308B (en
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文桂林
钱秀洋
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Hunan University
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Hunan University
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Abstract

The invention discloses a kind of impact resistant composite material fabric, this impact resistant composite material fabric is made up of steel wire mesh frame and the flexible fiber bundle be bundled on steel wire mesh frame.Impact resistant composite material fabric of the present invention effectively can prevent the Quick Extended of slippage between fiber and crackle, after avoiding fabric to be hit, mesh swells and is out of shape, heat conduction is good, high temperature resistant, can be widely used as the sandwich layer of anti-ballistic materials and the attaching parts of metal and nonmetallic materials.

Description

A kind of impact resistant composite material fabric
Technical field
The invention belongs to protective materials field, relate to a kind of impact resistant composite material fabric, particularly a kind of hybrid composite fabric preventing fiber slippage and cracking, can be applicable to the sandwich layer of anti-ballistic materials and the attaching parts of metal and nonmetallic materials.
Background technology
The shock resistance mechanism of high-performance fiber shock resistance fabric is mainly: when fiber is hit, shock wave energy rapid diffusion can be held, fibrous fracture time need absorb the energy that all will absorb alluvium in energy to failure, the distortion of sheet material integrally bending and the process such as interlayer slip thereof, these mechanism are common by the kinetic energy approach exhaustion of alluvium (as the swiftly passing object such as bullet, fragmentation), thus reach shock proof object.But by together with resin-bonded, very easily there is slippage when the thing that is hit impacts and loosen, causing rapid crack, shock wave energy diffusion hindered, cause high-performance fiber can not give full play to the advantage of self in fiber and fiber interweaving place.At present, mainly there are the following problems for composite shock resistance braided fabric: the position 1, be connected with metal parts is weaker, and poor thermal conductivity; 2, very easily there is slippage between fiber and loosen, the advantage of large energy when not giving full play to high-performance fiber fracture, can be absorbed.
Summary of the invention
The technical problem to be solved in the present invention overcomes the deficiencies in the prior art, particularly for the shortcoming of existing shock resistance fabric poor heat conductivity, non-refractory, connecting portion weakness, provide a kind of and effectively can prevent the Quick Extended of the slippage between fiber and crackle, avoid fabric to be hit after mesh swell and be out of shape, good, the resistant to elevated temperatures impact resistant composite material fabric of heat conduction.
For solving the problems of the technologies described above, the present invention by the following technical solutions:
A kind of impact resistant composite material fabric, described impact resistant composite material fabric is made up of steel wire mesh frame and the flexible fiber bundle be bundled on described steel wire mesh frame.
In above-mentioned impact resistant composite material fabric, preferably, described flexible fiber bundle is high-performance flexible fibre bundle, the TENSILE STRENGTH >=2000MPa of described high-performance flexible fibre bundle, fracture toughness >=1500mN/tex, elongation at break >=3%.
In above-mentioned impact resistant composite material fabric, preferred, the TENSILE STRENGTH of described high-performance flexible fibre bundle is 2500MPa ~ 3000MPa, and fracture toughness is 1500mN/tex ~ 2500mN/tex, and elongation at break is 3% ~ 5%.
In above-mentioned impact resistant composite material fabric, preferably, described flexible fiber bundle comprises one or more in nylon fiber, aramid fiber and ultra-high molecular weight polyethylene (UHMWPE) fiber.
In above-mentioned impact resistant composite material fabric, preferably, described flexible fiber bundle is bundled on described steel wire mesh frame in the mode of tangled up and knotted.
In above-mentioned impact resistant composite material fabric, preferably, described flexible fiber bundle weaves configuration in " N " type in the mesh cells of described steel wire mesh frame.
In above-mentioned impact resistant composite material fabric, preferably, described steel wire mesh frame is formed by steel alloy fibrage; The elastic modelling quantity of described steel alloy fiber is 200GPa ~ 210GPa, and shear strength is 450MPa ~ 600MPa, and heat resistance is 800 DEG C ~ 1000 DEG C.
In above-mentioned impact resistant composite material fabric, preferably, described steel alloy fiber is stainless steel fibre.
In above-mentioned impact resistant composite material fabric, preferably, the texture of weaving of described steel wire mesh frame comprises plain weave, twill or satin weave.
In the present invention, all scopes include endpoint value.
Principle of the present invention is as follows:
Tradition shock resistance fabric (as traditional shock resistance kevlar fabric) when being subject to impacting, failure mode main manifestations be the fracture of fiber and Fabric mesh distortion, swell, as shown in Figure 1.The fracture of fiber can absorb a large amount of energy, and this is favourable to shock resistance, but the distortion of Fabric mesh and swelling, make fabric lose impact resistance rapidly, thus make alluvium pass easily through fabric.The stressed schematic diagram of fabric unit as shown in Figure 2, single mesh cells (i.e. grid cell) is subject to the power F to surrounding extruding, due to the modulus of fabric and shear strength lower, fiber is wherein easy to deform and slippage (the A intertwined point in such as Fig. 2), can not give full play to the advantage of fiber; Meanwhile, when one of them mesh cells destroys, " reeling off raw silk from cocoons " phenomenon can occur, and the impact resistance of whole fabric declines rapidly, final generation moderate finite deformation and then inefficacy.
In order to improve the non-deformability of fabric, the stainless steel fibre braided fabric that hybrid composite fabric employing modulus provided by the invention is high, shearing strength is high, thermal conductivity is good or other steel alloy fibrous braid are skeleton, as shown in Figure 3 and Figure 4.When single mesh cells is subject to the power F to surrounding extruding, due to the modulus of fabric and shear strength higher, distortion is less likely to occur fiber wherein, shock wave energy rapid diffusion can be held, simultaneously the high-termal conductivity of stainless steel or other steel alloy heat rapid diffusion that impact can be made to produce, avoids local temperature rising.
But under larger extruding force F effect, still can there is slippage in fiber interweaving place, thus make mesh swell, and loses impact resistance; And when one of them mesh cells destroys, " reeling off raw silk from cocoons " phenomenon still can occur, the impact resistance of whole fabric also can decline rapidly.Therefore, the present invention considers stainless steel fibre intertexture place high-performance flexible fibre bundle to be carried out knotting binding, make slippage and cracking (such as bundling node 3 without slippage) no longer occur between fiber, each like this mesh cells also becomes independently unit, when one of them mesh cells destroys, other unit is unaffected, and this is also the basic reason that composite material fabric of the present invention has superior shock resistance.
The continuous winding weaving manner of high-performance flexible fibre bundle on steel wire, can not only improve intensity and the impact resistance of shock resistance fabric further, weaving of fabric can also be made to realize mechanized operation, thus realize industrialized mass production.One provided by the invention " N " type weaving manner as shown in Figure 4, high-performance flexible fibre bundle in independent mesh unit not only can improve the anti-extrusion ability of mesh greatly, the separate unit of quadrangle can be made to be partitioned into independent stable triangular structure unit further simultaneously, substantially increase the stability of fabric, thus play good shock resistance effect.
Compared with prior art, the invention has the advantages that:
1, the present invention adopts high-performance flexible fibre bundle to carry out tangled up and knotted binding at the intertexture place of steel alloy fiber reinforcement, each mesh of steel wire is made to become stable separate unit, effectively can prevent the Quick Extended of slippage between fiber and crackle, after avoiding fabric to be subject to bullet impact, mesh swells and is out of shape.
2, impact resistant composite material fabric of the present invention adopts steel alloy fibrage to become skeleton structure, has good, the resistant to elevated temperatures effect of heat conduction.
3, impact resistant composite material fabric of the present invention may be used for the parts preparing curved surface and other labyrinths, also can directly punch to be connected with miscellaneous part.
Accompanying drawing explanation
Fig. 1 is the failure mode schematic diagram of conventional fabrics when being hit.
Fig. 2 is the stressed schematic diagram of conventional fabrics when being hit.
Fig. 3 is the structural representation of the impact resistant composite material fabric of the embodiment of the present invention.
Fig. 4 is the stressed schematic diagram of mesh cells of the impact resistant composite material fabric of the embodiment of the present invention.
Fig. 5 is a kind of concrete structure schematic diagram that the impact resistant composite material fabric of the embodiment of the present invention is applied to impact-resistant panels.
Marginal data:
1, steel wire mesh frame; 2, high-performance flexible fibre bundle; 3, node is bundled; 4, " N " type weaving unit; 5, impact resistant composite material tissue layer; 6, sealer; 7, high impact resins layer.
Detailed description of the invention
Below in conjunction with Figure of description and concrete preferred embodiment, the invention will be further described, but protection domain not thereby limiting the invention.
The material adopted in following examples and instrument are commercially available.
embodiment:
A kind of impact resistant composite material fabric of the present invention, as shown in Figure 3, this impact resistant composite material fabric is made up of steel wire mesh frame 1 and the high-performance flexible fibre bundle 2 be bundled on steel wire mesh frame 1.
In the present embodiment, high-performance flexible fibre bundle 2 is " Kevlar-29 " aramid fiber, and TENSILE STRENGTH is 2800MPa, and fracture toughness is 2030mN/tex, and elongation at break is 3.8%.
In the present embodiment, high-performance flexible fibre bundle 2 is bundled on steel wire mesh frame 1 in the mode of tangled up and knotted, and steel wire mesh frame 1 is formed some binding nodes 3, in each mesh cells of steel wire mesh frame 1, form " N " type weaving unit 4.As shown in Figure 3, high-performance flexible fibre bundle 2 adopts " N " type continuous weaving in steel wire mesh frame 1, and " N " type structure of fibre bundle has two kinds, and one is perpendicular " N ", and one is horizontal " N ", is decided by woven mode, two kinds of structure alternately braidings.
In the present embodiment, steel wire mesh frame 1 is woven by stainless steel fibre to form; The elastic modelling quantity of stainless steel fibre is 207GPa, shear strength is 600MPa, heat resistance is 1000 DEG C.
In the present embodiment, the texture of weaving of steel wire mesh frame 1 is plain weave.
Impact resistant composite material fabric of the present invention is compared with the pure kevlar fabric of tradition; maximal destruction deflection can reduce 30%; more effectively protect personal safety; the energy absorbed during destruction can increase by 140%; can at 600 DEG C of temperature Long-Time Service; heat resistance can improve about 150%, has more superior protection effect.
Impact resistant composite material fabric of the present invention be can be applicable in impact-resistant panels; as the sandwich layer of impact-resistant panels; as shown in Figure 5, this impact-resistant panels comprises sealer 6(from top to bottom successively if rigidity is by bullet layer), impact resistant composite material tissue layer 5/ high impact resins layer 7(totally 6 cycles of being periodically alternately arranged), high impact resins layer 7(and layer 7 high impact resins layer) and sealer 6.
Impact resistant composite material fabric of the present invention can also be widely used in numerous anti-ballistic materials such as shock resistance plate, shock resistance armour plate, the shock resistance helmet or shock resistance shield, plays excellent shock resistance.
The above is only the preferred embodiment of the present invention, and protection scope of the present invention is also not only confined to above-described embodiment.All technical schemes belonged under thinking of the present invention all belong to protection scope of the present invention.It is noted that for those skilled in the art, improvements and modifications under the premise without departing from the principles of the invention, these improvements and modifications also should be considered as protection scope of the present invention.

Claims (9)

1. an impact resistant composite material fabric, is characterized in that, described impact resistant composite material fabric is made up of steel wire mesh frame and the flexible fiber bundle be bundled on described steel wire mesh frame.
2. impact resistant composite material fabric according to claim 1, it is characterized in that, described flexible fiber bundle is high-performance flexible fibre bundle, the TENSILE STRENGTH >=2000MPa of described high-performance flexible fibre bundle, fracture toughness >=1500mN/tex, elongation at break >=3%.
3. impact resistant composite material fabric according to claim 2, is characterized in that, the TENSILE STRENGTH of described high-performance flexible fibre bundle is 2500MPa ~ 3000MPa, and fracture toughness is 1500mN/tex ~ 2500mN/tex, and elongation at break is 3% ~ 5%.
4. the impact resistant composite material fabric according to any one of claims 1 to 3, is characterized in that, described flexible fiber bundle comprise in nylon fiber, aramid fiber and superhigh molecular weight polyethylene fibers one or more.
5. the impact resistant composite material fabric according to any one of claims 1 to 3, is characterized in that, described flexible fiber bundle is bundled on described steel wire mesh frame in the mode of tangled up and knotted.
6. impact resistant composite material fabric according to claim 5, is characterized in that, described flexible fiber bundle weaves configuration in " N " type in the mesh cells of described steel wire mesh frame.
7. the impact resistant composite material fabric according to any one of claims 1 to 3, is characterized in that, described steel wire mesh frame is formed by steel alloy fibrage; The elastic modelling quantity of described steel alloy fiber is 200GPa ~ 210GPa, and shear strength is 450MPa ~ 600MPa, and heat resistance is 800 DEG C ~ 1000 DEG C.
8. impact resistant composite material fabric according to claim 7, is characterized in that, described steel alloy fiber is stainless steel fibre.
9. impact resistant composite material fabric according to claim 7, is characterized in that, the texture of weaving of described steel wire mesh frame comprises plain weave, twill or satin weave.
CN201510699630.7A 2015-10-26 2015-10-26 A kind of impact resistant composite material fabric Expired - Fee Related CN105220308B (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109183426A (en) * 2018-08-28 2019-01-11 深圳市辰越科技有限公司 A kind of amorphous alloy stab-resistance body armor and preparation method thereof
CN111101261A (en) * 2019-12-09 2020-05-05 常州凯丽特装饰材料有限公司 Preparation method of textile composite material for protecting low-speed impact

Citations (7)

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US6247298B1 (en) * 1996-02-01 2001-06-19 N.V. Bekaert S.A. Stab-resistant insert for protective textile
CN1429292A (en) * 2000-05-11 2003-07-09 贝克特股份有限公司 Cut resistant fabric for protective textiles
CN101858076A (en) * 2009-04-07 2010-10-13 常州市永新华立纺织复合材料有限公司 High-strength warp knitting geogrid
CN101977762A (en) * 2008-02-22 2011-02-16 罗拉斯托普有限公司 Reinforced material
CN102470700A (en) * 2009-07-27 2012-05-23 N.V.贝卡特股份有限公司 Hybrid steel-textile reinforcement ply for radial tires
CN103334213A (en) * 2013-05-16 2013-10-02 江南大学 Quasi-all-carbon fiber biaxial weft-knitted fabric bound by pre-oxidized fibers
CN103866472A (en) * 2012-12-13 2014-06-18 江南大学 Integral pyramid wire frame structured woven fabric

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6247298B1 (en) * 1996-02-01 2001-06-19 N.V. Bekaert S.A. Stab-resistant insert for protective textile
CN1429292A (en) * 2000-05-11 2003-07-09 贝克特股份有限公司 Cut resistant fabric for protective textiles
CN101977762A (en) * 2008-02-22 2011-02-16 罗拉斯托普有限公司 Reinforced material
CN101858076A (en) * 2009-04-07 2010-10-13 常州市永新华立纺织复合材料有限公司 High-strength warp knitting geogrid
CN102470700A (en) * 2009-07-27 2012-05-23 N.V.贝卡特股份有限公司 Hybrid steel-textile reinforcement ply for radial tires
CN103866472A (en) * 2012-12-13 2014-06-18 江南大学 Integral pyramid wire frame structured woven fabric
CN103334213A (en) * 2013-05-16 2013-10-02 江南大学 Quasi-all-carbon fiber biaxial weft-knitted fabric bound by pre-oxidized fibers

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109183426A (en) * 2018-08-28 2019-01-11 深圳市辰越科技有限公司 A kind of amorphous alloy stab-resistance body armor and preparation method thereof
CN111101261A (en) * 2019-12-09 2020-05-05 常州凯丽特装饰材料有限公司 Preparation method of textile composite material for protecting low-speed impact

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